5’s Flashcards

(51 cards)

1
Q

Engine oil pressure limits

A

Pressure limits for:

NG at ground idle - 5 psi
NG 80% to 95% - 32 psi
NG equal to or greater than 95% - 50 psi
Normal operation - 35 to 90 psi
Maximum for contingency power - 110 psi
Maximum for cold weather starts - 150 psi
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2
Q

Max engine oil temperature (at what temperature does caution activate)?

A

149 C

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3
Q

ENG XMSN oil temperature limits.

Caution vs Warning

A

Caution activates greater than 140 C

Warning activates greater than 190 C

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4
Q

XMSN oil temperature limits. (At what temperature does caution activate)?

A

Greater than 140 C

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5
Q

XMSN oil pressure limits.

A

Minimum at ground idle- 7 psi
Minimum at 100% NR - 20 psi
Normal operation - 20 to 90 psi

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6
Q

Flight Control Hydraulic Pressure normal operating range

A

2,500 to 3,200 psi

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7
Q

Utility System Hydraulic Pressure normal operating range

A

2,500 to 3,500 psi

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8
Q

Hydraulic system temperature,

Cautionary range and max

A

Caution range 95-120 C

Max 120 C

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9
Q

Rotor speed limitations

A
Minimum transient power on- 91%
Transient - 91% to 97%
Normal range - 97% to 101%
Transient - 101% to 106%
Max power on - 106%
Max autorotation - 108%
*Maximum transient* - Max Transient per Table 5-5 is 111%. 111.5% only pertains to the note regarding the 2408-13-1 entry requirements.
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10
Q

Should NR exceed _____% but not ____%, no entry need be made on a form (BONUS), but willful operation will not be conducted in this range.

A

108%, 111.5%, DA Form 2408-13-1

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11
Q

CGI ranges

A

Green - normal operation
Yellow - transient
Red - avoid
White - test

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12
Q

Flight with NR equal to or less than ____% with an inoperative CGI is ________.

A

98%, prohibited

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13
Q

Any excursion into the red or yellow band of the CGI for more than ____________ requires and entry on DA Form 2408-13-1.

A

45 seconds

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14
Q

The APU shall not be started with a tailwind in excess of ________knots.

A

25 knots

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15
Q

Main engines shall not be started with a tailwind in excess of ________knots.

A

10 knots

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16
Q

If it becomes necessary to shutdown outside of [tail] wind limits shown in figure 5-6 or 5-7, the following precautions are recommended:

A

Aircraft should land in an area which is

  • clear
  • level as possible
  • at least 300 feet away from verticals obstructions
  • positioned so that wind is coming at the aircraft from the left side
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17
Q

PTIT Limits

A

MAX continuous- up to 816 C

30 minutes - 816 to 854 C

10 minute - 854 to 899 C

2.5 minute(contingency)- 899 to 932 C

12 seconds (MAX TRANS)- 932 to 943 C

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18
Q

NG limits

A

Ground idle minimum- 50%

Maximum- 111%

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19
Q

Max NP speed (%)

A

111.5%

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20
Q

Only those fuels listed in ______________ shall be used. Emergency fuel shall not be used for more than ________ cumulative time

A

Chapter 2

6 hours

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21
Q

Max GWT

22
Q

Cargo hook(s) limitations

A

FWD or AFT hooks- 17k
Tandem load- 25k
Center hook- 26k

23
Q

When a combination of internal and external loads are carried on the same flight and external load exceeds _________ pounds, internal load should be positioned forward of the ________.

A

12k

Utility hatch

24
Q

Cargo Winch weight limitations

A

The cargo winch is rated at 3,000 lbs straight pull. With one pulley the mechanical advantage is doubled to 6,000 lbs. 2 pulleys gets you 9,000 lbs and 3 pulleys the grand total of 12,000 lbs. 5-4 Helicopter Loading Limits paragraph d. (PDF Page 711)

25
The rescue winch is limited to a maximum load of _____ pounds.
600 lbs
26
Maximum crosswind or sideward flight is ___knots
45 knots
27
Maximum airspeed rearward flight
40 knots
28
Maximum tailwind during hover
40 knots
29
Max airspeed with lower section of cabin entrance door open and locked
60 KCAS
30
Rescue hatch shall not be opened or closed above ________KCAS
90 KCAS
31
Upper section of cabin entrance door may only be closed below ________KCAS
100 KCAS
32
*CAUTION* | A dual _______ primary channel failure may occur when in rearward flight or a tailwind in excess of ______ knots.
FADEC | 40 knots
33
If a sling or hook should fail while carrying a tandem load, limit airspeed to a maximum of:
60 KCAS
34
Airspeed limits: Single DAFCS DAFCS Off
Single -100 KCAS or VNE | Both off- 160 KCAS or VNE, provided DAFCS are turned off below 100 KCAS
35
Aerobatics are prohibited with this helicopter. Aerobatics are defined as intentional maneuvers beyond:
30 degrees pitch | 60 degrees roll
36
When operating with BALT/RALT engaged, limit bank angles to _____degrees maximum
45 degreees
37
Maximum speed for roll on landings Maximum nose up attitude
60 KGS 20 degrees
38
Maximum rates of descent
Up to 33k lbs-492 ft/min 33k to 40k- 450 ft/min Greater than 40k lbs-360ft/min
39
Ground operation limitations
0.75” pedal input 1” lateral cyclic 2” aft cyclic Thrust control lever no lower than ground detent
40
When will a blade watcher and taxi director be positioned?
- When ground taxiing less than 75’ from an obstruction | - on an unimproved or unfamiliar airfield not designated for CH47’s
41
The CH47 is qualified for flight in instrument meteorological conditions provided the following exist:
- both DAFCS are operational - SFD’s are operating - three MFD’s, two CDU’s, two GPPU’s, two DCU’s, two EGI’s, two ADC’s are operational * MFD 1 and 4 are mandatory with the third MFD being either 2 or 3. MFD 5 is optional. 5-7 Helicopter Environmental Restrictions paragraph b. (PDF page 719)*
42
Coupled ILS approaches at localizer intercept angles of greater than ______ degrees are prohibited.
60 degrees
43
Shock absorber vent valves | Temperatures for operation
Open for operation- below (minus) -18 C Closed for operation- above (minus) -1 C
44
Max airspeed with skis
130 KCAS or VNE
45
Max rates of descent *with skis* + taxi speed
Up to 33k-480 ft/min 46k to 50k- 240 ft/min Maximum taxi speed is 5KGS
46
Windshield heat shall not be used above ________ C.
24 C
47
Maximum rate for pressure refueling
300 gal/min at 55 psi -10, pg. 2-45
48
The maximum internal pressure of ERFS II tank
5 psi
49
How many first aid kits are on board a 47?
7
50
How many first aid kits are required to fly?
1-services 5 crew members
51
When will the emergency lights come on?
1) loss of electrical power | 2) landing in excess of 3-4 G’s